Investigation at low speeds of deflectors and spoilers as gust alleviators on a model of the Bell X-5 airplane with 35 degrees swept wings on a high-aspect-ratio 35 degree swept-wing - fuselage model /
Results of an investigation at low speeds to determine the gust-alleviation capabilities (reduction in lift-curve slope) of spoilers and deflectors on a 35 degree swept-wing model of high aspect ratio and on a 1/4-scale model of the X-5 airplane with 35 degree swept wings indicate that deflector and...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington :
National Advisory Committee for Aeronautics,
[1957]
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
4057 |
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| Call Number: |
NACA TN 4057 |
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